GOE 500 AIRFOIL (goe500-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 500 AIRFOIL (goe500-il) Reynolds number: 100,000 Max Cl/Cd: 65.62 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe500-il-100000-n5.txt Download as CSV file: xf-goe500-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 500 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.250 -0.2282 0.09355 0.08859 -0.0633 0.9681 0.0450
-8.000 -0.2166 0.08975 0.08478 -0.0675 0.9633 0.0466
-7.750 -0.2121 0.08624 0.08128 -0.0701 0.9560 0.0469
-7.500 -0.2039 0.08217 0.07721 -0.0742 0.9497 0.0468
-7.250 -0.1981 0.07815 0.07320 -0.0776 0.9414 0.0469
-7.000 -0.1846 0.07274 0.06777 -0.0849 0.9347 0.0482
-6.750 -0.1765 0.06626 0.06126 -0.0932 0.9254 0.0494
-6.500 -0.1522 0.05522 0.05006 -0.1097 0.9188 0.0500
-6.250 -0.1272 0.04372 0.03818 -0.1256 0.9104 0.0516
-6.000 -0.0982 0.04266 0.03705 -0.1278 0.9060 0.0538
-5.750 -0.0522 0.03373 0.02718 -0.1414 0.9032 0.0562
-5.500 -0.0099 0.02935 0.02194 -0.1478 0.9014 0.0594
-5.250 0.0105 0.02752 0.01967 -0.1478 0.8933 0.0618
-5.000 0.0439 0.02642 0.01842 -0.1495 0.8898 0.0639
-4.750 0.0801 0.02519 0.01693 -0.1516 0.8874 0.0665
-4.500 0.1062 0.02422 0.01571 -0.1517 0.8814 0.0694
-4.250 0.1358 0.02335 0.01458 -0.1523 0.8763 0.0736
-4.000 0.1699 0.02282 0.01401 -0.1536 0.8731 0.0787
-3.750 0.2063 0.02195 0.01289 -0.1552 0.8708 0.0851
-3.500 0.2259 0.02166 0.01262 -0.1539 0.8621 0.0900
-3.250 0.2596 0.02108 0.01188 -0.1549 0.8585 0.1003
-3.000 0.2958 0.02055 0.01124 -0.1564 0.8558 0.1139
-2.750 0.3167 0.02026 0.01099 -0.1552 0.8462 0.1244
-2.500 0.3526 0.01968 0.01037 -0.1565 0.8420 0.1395
-2.250 0.3764 0.01943 0.01012 -0.1557 0.8329 0.1526
-2.000 0.4099 0.01899 0.00966 -0.1565 0.8280 0.1684
-1.750 0.4355 0.01879 0.00948 -0.1560 0.8203 0.1827
-1.250 0.4976 0.01815 0.00888 -0.1568 0.8101 0.2187
-1.000 0.5216 0.01804 0.00885 -0.1561 0.8017 0.2429
-0.750 0.5546 0.01770 0.00856 -0.1567 0.7973 0.2782
-0.500 0.5788 0.01766 0.00858 -0.1560 0.7888 0.3119
-0.250 0.6107 0.01741 0.00838 -0.1565 0.7834 0.3522
0.000 0.6374 0.01734 0.00838 -0.1561 0.7759 0.3893
0.250 0.6674 0.01717 0.00827 -0.1562 0.7694 0.4289
0.500 0.6959 0.01705 0.00823 -0.1561 0.7624 0.4680
0.750 0.7242 0.01691 0.00819 -0.1560 0.7549 0.5142
1.000 0.7527 0.01670 0.00815 -0.1558 0.7479 0.5807
1.250 0.7784 0.01640 0.00813 -0.1550 0.7399 0.6785
1.500 0.8055 0.01587 0.00795 -0.1543 0.7325 1.0000
1.750 0.8341 0.01595 0.00793 -0.1542 0.7240 1.0000
2.000 0.8622 0.01605 0.00795 -0.1541 0.7154 1.0000
2.250 0.8919 0.01610 0.00792 -0.1542 0.7072 1.0000
2.500 0.9182 0.01628 0.00806 -0.1538 0.6979 1.0000
2.750 0.9489 0.01633 0.00804 -0.1541 0.6902 1.0000
3.000 0.9735 0.01656 0.00826 -0.1534 0.6795 1.0000
3.250 1.0013 0.01671 0.00839 -0.1533 0.6704 1.0000
3.500 1.0286 0.01688 0.00854 -0.1530 0.6610 1.0000
3.750 1.0539 0.01713 0.00880 -0.1525 0.6509 1.0000
4.000 1.0823 0.01728 0.00894 -0.1524 0.6421 1.0000
4.250 1.1067 0.01756 0.00925 -0.1517 0.6314 1.0000
4.500 1.1322 0.01782 0.00954 -0.1512 0.6216 1.0000
4.750 1.1598 0.01803 0.00976 -0.1509 0.6127 1.0000
5.000 1.1829 0.01836 0.01015 -0.1501 0.6013 1.0000
5.250 1.2069 0.01863 0.01046 -0.1492 0.5893 1.0000
5.500 1.2307 0.01889 0.01073 -0.1483 0.5762 1.0000
5.750 1.2550 0.01916 0.01104 -0.1475 0.5642 1.0000
6.000 1.2782 0.01949 0.01144 -0.1466 0.5528 1.0000
6.250 1.2997 0.01982 0.01182 -0.1453 0.5387 1.0000
6.500 1.3202 0.02012 0.01211 -0.1438 0.5212 1.0000
6.750 1.3369 0.02049 0.01251 -0.1417 0.4994 1.0000
7.000 1.3529 0.02090 0.01285 -0.1394 0.4757 1.0000
7.250 1.3673 0.02140 0.01334 -0.1370 0.4524 1.0000
7.500 1.3809 0.02198 0.01385 -0.1345 0.4287 1.0000
7.750 1.3924 0.02262 0.01449 -0.1317 0.4038 1.0000
8.000 1.4014 0.02331 0.01519 -0.1286 0.3782 1.0000
8.250 1.4087 0.02410 0.01598 -0.1253 0.3471 1.0000
8.500 1.4123 0.02513 0.01689 -0.1216 0.3046 1.0000
8.750 1.4081 0.02672 0.01814 -0.1173 0.2522 1.0000
9.000 1.4019 0.02873 0.01981 -0.1131 0.2041 1.0000
9.250 1.3954 0.03101 0.02178 -0.1093 0.1524 1.0000
9.500 1.3886 0.03349 0.02397 -0.1058 0.1145 1.0000
9.750 1.3855 0.03581 0.02617 -0.1029 0.0923 1.0000
10.000 1.3846 0.03804 0.02838 -0.1004 0.0793 1.0000
10.250 1.3852 0.04023 0.03060 -0.0981 0.0712 1.0000
10.500 1.3837 0.04268 0.03306 -0.0960 0.0656 1.0000
10.750 1.3859 0.04489 0.03540 -0.0942 0.0610 1.0000
11.000 1.3860 0.04737 0.03796 -0.0926 0.0571 1.0000
11.250 1.3826 0.05029 0.04090 -0.0909 0.0541 1.0000
11.500 1.3853 0.05269 0.04348 -0.0896 0.0511 1.0000
11.750 1.3868 0.05529 0.04621 -0.0884 0.0483 1.0000
12.000 1.3868 0.05810 0.04910 -0.0874 0.0458 1.0000
12.250 1.3855 0.06116 0.05220 -0.0863 0.0436 1.0000
12.500 1.3907 0.06358 0.05480 -0.0853 0.0415 1.0000
12.750 1.3952 0.06612 0.05748 -0.0845 0.0392 1.0000
13.000 1.3990 0.06879 0.06022 -0.0838 0.0371 1.0000
13.250 1.4028 0.07150 0.06293 -0.0830 0.0353 1.0000
13.500 1.4110 0.07382 0.06539 -0.0821 0.0338 1.0000
13.750 1.4181 0.07634 0.06812 -0.0814 0.0321 1.0000
14.000 1.4235 0.07907 0.07101 -0.0809 0.0305 1.0000
14.250 1.4277 0.08190 0.07396 -0.0806 0.0291 1.0000
14.500 1.4331 0.08464 0.07673 -0.0803 0.0279 1.0000
14.750 1.4398 0.08751 0.07975 -0.0798 0.0270 1.0000
15.000 1.4416 0.09106 0.08361 -0.0797 0.0261 1.0000
15.250 1.4410 0.09495 0.08778 -0.0799 0.0253 1.0000
15.500 1.4384 0.09907 0.09216 -0.0805 0.0245 1.0000
15.750 1.4341 0.10346 0.09677 -0.0815 0.0237 1.0000
16.000 1.4292 0.10795 0.10146 -0.0828 0.0231 1.0000
16.250 1.4242 0.11249 0.10618 -0.0843 0.0226 1.0000
16.500 1.4191 0.11715 0.11099 -0.0861 0.0221 1.0000
16.750 1.4145 0.12181 0.11579 -0.0879 0.0217 1.0000
17.000 1.4090 0.12677 0.12092 -0.0900 0.0214 1.0000
17.250 1.3963 0.13338 0.12777 -0.0934 0.0213 1.0000
17.500 1.3808 0.14083 0.13549 -0.0978 0.0212 1.0000
17.750 1.3645 0.14884 0.14372 -0.1028 0.0212 1.0000
18.000 1.3470 0.15757 0.15268 -0.1086 0.0212 1.0000
18.250 1.3289 0.16700 0.16232 -0.1151 0.0212 1.0000
18.500 1.3094 0.17756 0.17306 -0.1226 0.0213 1.0000
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